Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10357
Reference26 articles.
1. Conical similarity of shock/boundary-layer interactions generated byswept and unswept fins
2. Spanwise propagation of upstream influence in conical swept shock/boundary-layer interactions
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